View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 65963U 26144.88519644 +.00000000 +00000-0 +19930-3 0 00009
2 65963 51.9038 8.6931 0000764 108.9426 251.1620 14.79937432 07
| Epoch (UTC): | 24 May 2026 21:14:40 |
| Eccentricity: | 0.0000764 |
| inclination: | 51.9038° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 8.6931° |
| argument of perigee: | 108.9426° |
| revolutions per day: | 14.79937432 |
| mean anomaly at epoch: | 251.1620° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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